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61. 发明申请

US20090134273A1 UNMANNED AERIAL VEHICLE AND LAUNCH ASSEMBLY 有权
标题翻译：无人驾驶的航空母舰和发射装置
公开(公告)号：US20090134273A1
公开(公告)日：2009-05-28
申请号：US11064287
申请日：2005-02-22
申请人： Mark A. Page , Doug McLarty , Adrian Fazio , Christian Durand , Bob Emerick
发明人： Mark A. Page , Doug McLarty , Adrian Fazio , Christian Durand , Bob Emerick
IPC分类号： B64C1/00 , B28B5/00 , B64F1/04
CPC分类号： B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/082 , B64C2201/084 , B64C2201/165 , B64C2201/201
摘要： An unmanned aerial vehicle (UAV) is provided, that is cost effective to use and manufacture and that includes a low count of component parts, allowing mission planners to use the UAVs in a disposable manner. The UAV includes an airframe having a central body and wings extending from the central body, defining an interior cavity. The airframe includes an upper and a lower shell, each configured of a unitary piece of plastic. The upper and lower shells have walls among them that define a fuel tank and a payload bay in a stacked configuration. The airframe can further include a payload cover configured to enclose the payload bay and to contribute to the central body of the airframe. A launch assembly is also provided. In a first configuration, a launch assembly is provided, that includes a container for housing multiple UAVs and a deployment mechanism that initiates rapid ejection of the UAVs from the container. In a second configuration, a launch assembly is provided, that includes an elastic tether connecting a UAV to an accelerated mass for gentle acceleration to flight speed under a stable tow.
摘要翻译：提供无人驾驶飞行器（UAV），使用和制造具有成本效益，并且包括低数量的部件，允许任务规划人员以一次性方式使用无人机。无人机包括具有中心体的机身和从中心体延伸的翼，限定内腔。机身包括一个上部和下部壳体，每个都由整体塑料构成。上壳体和下壳体之间具有限定了堆叠构造的燃料箱和有效载荷的壁。机身还可以包括配置成包围有效载荷舱并有助于机身的中心体的有效载荷盖。还提供发射组件。在第一配置中，提供了一种发射组件，其包括用于容纳多个UAV的容器和启动无人机从容器的快速喷射的展开机构。在第二构造中，提供了一种发射组件，其包括将UAV连接到加速质量块的弹性系绳，以在稳定的丝束下平缓加速到飞行速度。

62. 发明申请

US20090045295A1 Vertical/Short Take-Off and Landing Aircraft 有权
标题翻译：垂直/短时起飞和着陆飞机
公开(公告)号：US20090045295A1
公开(公告)日：2009-02-19
申请号：US11838731
申请日：2007-08-14
申请人： Gert Lundgren
发明人： Gert Lundgren
IPC分类号： G05D1/08 , B64C27/22
CPC分类号： B64C29/0033 , B64C39/024 , B64C39/04 , B64C2201/042 , B64C2201/044 , B64C2201/088 , B64C2201/165
摘要： A vertical/short take-off and landing aircraft with a single proprotor assembly that has a pair of inline counter-rotating rotors. Two inline counter-rotating engines are directly connected to the rotors. One engine is shut down in horizontal flight to improve efficiency. Gimbal mounting the proprotor assembly permits thrust to be directed forward to back and left to right to control pitch and roll when hovering. Varying the relative engine speeds controls yaw. The aircraft is adaptable as an unmanned vehicle.
摘要翻译：具有单个推进器组件的垂直/短距起飞和着陆飞机，其具有一对在线的反向旋转的转子。两个直列反向旋转发动机直接连接到转子上。一个引擎在水平飞行中关闭以提高效率。安装推进器组件的万向节允许推动力向前指向前向左并向左转，以便在悬停时控制俯仰和滚动。改变相对发动机转速来控制偏航。该飞机适用于无人驾驶的车辆。

63. 发明申请

US20080210818A1 Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV) 审中-公开
标题翻译：自主的，可回填计算机控制的无人机（UAV）
公开(公告)号：US20080210818A1
公开(公告)日：2008-09-04
申请号：US11822278
申请日：2007-07-03
申请人： Tien-Seng Chiu , Jay Willmott , Kirk Jenkins
发明人： Tien-Seng Chiu , Jay Willmott , Kirk Jenkins
IPC分类号： B64C1/00 , B64C1/10 , A45C5/00
CPC分类号： B64C1/00 , A45C5/00 , A45C13/02 , B64C1/30 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/126 , B64C2201/127 , B64C2201/141 , B64C2201/165 , B64C2201/187 , B64C2201/201 , B64C2201/203
摘要： A modular unmanned aerial vehicle (UAV) having a fuselage, a nose cone, a left wing piece, a right wing piece, and a tail section. The tail section and nose cone each join to the fuselage through mating bulkhead structures that provide quick connection capability while being readily separated so as to enable the UAV to break apart at these connection points and thereby absorb or dissipate impact upon landing. The UAV is capable of rapid assembly in the field for two-man launch and data retrieval, as well as quick disassembly into these five component parts for transport and storage in a highly compact transport case that can be carried as a backpack.
摘要翻译：具有机身，鼻锥，左翼片，右翼片和尾部的模块化无人驾驶飞行器（UAV）。尾部和鼻锥每个通过配合的隔板结构连接到机身，提供快速的连接能力，同时易于分离，以便使UAV在这些连接点处分裂，从而吸收或消散着陆时的冲击。无人机能够在现场快速组装两人发射和数据检索，以及快速拆卸到这五个部件中，用于运输和存储，可以作为背包携带的高度紧凑的运输箱。

64. 发明授权

US07364114B2 Aircraft 有权
标题翻译：飞机
公开(公告)号：US07364114B2
公开(公告)日：2008-04-29
申请号：US10934634
申请日：2004-09-03
申请人： Aloys Wobben
发明人： Aloys Wobben
IPC分类号： B64C29/00
CPC分类号： B64C39/024 , B64C27/20 , B64C29/00 , B64C39/022 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/165 , B66F19/00
摘要： The present invention concerns an aircraft having a plurality of lifting and thrust rotors, with an electric motor and an inverter for each motor. In order to provide an aircraft having a greater payload, connecting bars are provided between the motors. In that respect the invention is based on the realization that, if such connecting bars are arranged in the manner of a latticework, they can provide a light but nonetheless stable structure for the aircraft, and that structure can carry correspondingly greater loads.
摘要翻译：本发明涉及具有多个提升和推力转子的飞行器，其中每个马达具有电动马达和逆变器。为了提供具有更大有效载荷的飞行器，在马达之间提供连接杆。在这方面，本发明基于如下认识：如果这种连接杆以网格的方式布置，则它们可以为飞行器提供轻但是稳定的结构，并且该结构可承载较大的载荷。

65. 发明申请

US20070034737A1 Dual axis control for cycloidal propeller 审中-公开
标题翻译：摆线螺旋桨双轴控制
公开(公告)号：US20070034737A1
公开(公告)日：2007-02-15
申请号：US11200319
申请日：2005-08-09
申请人： Glenn Tierney
发明人： Glenn Tierney
IPC分类号： B64C39/00
CPC分类号： B64C39/005 , B64B1/30 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102 , B64C2201/104 , B64C2201/165
摘要： A system and method for moving an aerial vehicle along a flight path includes rotatable hubs mounted on opposite sides of the vehicle. Elongated airfoils are mounted on the hubs parallel to a common hub axis for rotation about the hub axis on a blade path. Each airfoil defines a chord line and the system includes a gear assembly changeable, during hub rotation, between a first modality wherein airfoil chord lines remain tangential to the blade path (curtate flight), and a second modality wherein airfoil chord lines remain parallel to the flight path of the vehicle (prolate flight). Also, rotation of the hub can be stopped and the airfoils used for fixed wing flight.
摘要翻译：沿着飞行路径移动飞行器的系统和方法包括安装在车辆的相对侧上的可旋转轮毂。细长的翼型件平行于公共轮毂轴线安装在轮毂上，以便在叶片路径上围绕轮毂轴线旋转。每个翼型件限定弦线，并且该系统包括齿轮组件，在轮毂旋转期间，其中翼型弦线保持与叶片路径相切的第一模态（curtate飞行）和第二模态，其中翼型弦线保持平行于车辆的飞行路线（长跑）。此外，轮毂的旋转可以停止，翼型件用于固定翼飞行。

66. 发明申请

US20060231675A1 Gyro-stabilized air vehicle 有权
公开(公告)号：US20060231675A1
公开(公告)日：2006-10-19
申请号：US11384167
申请日：2006-03-17
申请人： Nicolae Bostan
发明人： Nicolae Bostan
IPC分类号： B64C29/00
CPC分类号： B64C3/385 , B64C17/06 , B64C27/20 , B64C29/0033 , B64C29/02 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/127 , B64C2201/146 , B64C2201/162 , B64C2201/165 , Y02T50/14
摘要： A vertical takeoff and landing (VTOL) air vehicle disclosed. The air vehicle can be manned or unmanned. In one embodiment, the air vehicle includes two shrouded propellers, a fuselage and a gyroscopic stabilization disk installed in the fuselage. The gyroscopic stabilization disk can be configured to provide sufficient angular momentum, by sufficient mass and/or sufficient angular velocity, such that the air vehicle is gyroscopically stabilized during various phases of flight. In one embodiment the fuselage is fixedly attached to the shrouded propellers. In another embodiment, the shrouded propellers are pivotably mounted to the fuselage.

67. 发明授权

US07097137B2 Launch and recovery system for unmanned aerial vehicles 有权
标题翻译：无人机的发射和恢复系统
公开(公告)号：US07097137B2
公开(公告)日：2006-08-29
申请号：US10754251
申请日：2004-01-09
申请人： William R. McDonnell
发明人： William R. McDonnell
IPC分类号： B64F1/02
CPC分类号： B64F1/02 , B64C25/68 , B64C39/024 , B64C2201/084 , B64C2201/104 , B64C2201/165 , B64C2201/182 , B64C2201/205 , B64D3/00 , B64F1/04 , B64F1/10
摘要： A method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10). The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).
摘要翻译：一种发射和检索无人机（无人机）的方法（10）。优选的发射方法是将无人机（10）运送到高度，使用类似于用来搭载高层游客的伞（8）。无人机被丢弃，并在潜水中获得足够的空速，执行上升到等级控制飞行。回收的首选方法是使UAV飞入并锁定在悬挂拖线（4）上或悬挂在拖绳上的电缆，然后被绞盘回到船（2）。

68. 发明授权

US07090166B2 Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for transmitting forces to the aircraft during launch 有权
标题翻译：用于发射无人机的方法和装置，包括在发射期间向飞机传递力的方法和装置
公开(公告)号：US07090166B2
公开(公告)日：2006-08-15
申请号：US10758948
申请日：2004-01-16
申请人： Brian D. Dennis , Andreas H. von Flotow
发明人： Brian D. Dennis , Andreas H. von Flotow
IPC分类号： B64F1/06
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64F1/06
摘要： Methods and apparatuses for launching unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be launched from an apparatus that includes an extendable boom. A launch carriage is positioned on a launch guide structure of the boom and carries the aircraft during takeoff. An energy reservoir is configured to provide energy to the launch carriage during takeoff of the aircraft, and can absorb energy from the launch carriage to decelerate the launch carriage after takeoff. The apparatus can further include a transmission that smoothly and rapidly accelerates and/or decelerates the launch carriage.
摘要翻译：描述了发射无人机和其他飞行装置或射弹的方法和装置。在一个实施例中，飞行器可以从包括可扩展起重臂的装置发射。发射架位于起重臂的发射导向结构上，并在起飞时承载飞机。能量储存器构造成在飞行器起飞期间向发射台提供能量，并且可以从起飞台吸收能量，以在起飞后减速发射台。该装置还可以包括使发射台平滑且快速地加速和/或减速的变速器。

69. 发明授权

US07059564B2 Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line 有权
标题翻译：用于捕获和恢复无人机的方法和装置，包括用于在线上捕获飞机的防滑板
公开(公告)号：US07059564B2
公开(公告)日：2006-06-13
申请号：US10758940
申请日：2004-01-16
申请人： Brian D. Dennis
发明人： Brian D. Dennis
IPC分类号： B64F1/02
CPC分类号： B64F1/06 , B63B27/26 , B64C39/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/084 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64F1/04
摘要： Methods and apparatuses for capturing and recovering unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be captured by a recovery line in flight, a process that can be aided by a line capture device having a retainer with two portions spaced apart by a distance great enough to receive the recovery line, e.g., to capture the recovery line with increased security. The line capture device can be operatively mounted on a lifting surface of the aircraft.
摘要翻译：描述了用于捕获和恢复无人驾驶飞机和其他飞行装置或射弹的方法和装置。在一个实施例中，飞行器可以由飞行中的恢复线捕获，该过程可以由具有保持器的线捕获装置辅助，该保持器具有两个间隔开足够大的距离以接收恢复线，例如捕获恢复线增加了安全性。线捕获装置可以可操作地安装在飞行器的提升表面上。

70. 发明授权

US07055777B2 Airship and method of operation 失效
标题翻译：飞艇及作战方法
公开(公告)号：US07055777B2
公开(公告)日：2006-06-06
申请号：US10178345
申请日：2002-06-25
申请人： Hokan S. Colting
发明人： Hokan S. Colting
IPC分类号： B64B1/02 , B64B1/24
CPC分类号： B64B1/34 , B64B1/02 , B64B1/32 , B64C21/02 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/044 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/146 , B64C2201/165 , Y02T50/166
摘要： An airship has a generally spherical shape and has an internal envelope for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7% full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.
摘要翻译：飞艇具有大致球形并且具有用于容纳诸如氦气或氢气的提升气体的内部信封。飞艇有一个推进和控制系统，允许飞行到所需的游荡地点，并在该地点保持一段时间。在一个实施例中，当内部信封充满提升气体的时间少至7％时，飞艇可以达到中性浮力，并且可以具有大约6万英尺的服务天花板。飞艇具有可以包括通信设备或监视的设备模块设备，或两者兼而有之。飞艇可以从地面站遥控。飞艇具有太阳能电池阵列，推进和控制系统的电动机由阵列获得的功率驱动。飞艇还具有可用于驱动电动机的辅助动力单元。飞艇可以有一个推动螺旋桨，有助于驾驶飞艇，还可以使球形飞艇进一步向后流动。在一个实施例中，飞艇可以在高度加油以允许延长的游荡。

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